High performance parallel computing of flows in complex geometries: I. methods N Gourdain, L Gicquel, M Montagnac, O Vermorel, M Gazaix, ... Computational Science & Discovery 2 (1), 015003, 2009 | 199* | 2009 |
Effects of free-stream turbulence on high pressure turbine blade heat transfer predicted by structured and unstructured LES EC Morata, N Gourdain, F Duchaine, LYM Gicquel International Journal of Heat and Mass Transfer 55 (21-22), 5754-5768, 2012 | 123 | 2012 |
Large eddy simulation of flows in industrial compressors: a path from 2015 to 2035 N Gourdain, F Sicot, F Duchaine, L Gicquel Philosophical Transactions of the Royal society A: Mathematical, Physical …, 2014 | 117 | 2014 |
High performance parallel computing of flows in complex geometries LYM Gicquel, N Gourdain, JF Boussuge, H Deniau, G Staffelbach, P Wolf, ... Comptes Rendus Mécanique 339 (2-3), 104-124, 2011 | 109 | 2011 |
Unsteady simulation of an axial compressor stage with casing and blade passive treatments N Gourdain, F Leboeuf | 109 | 2009 |
Simulation of rotating stall in a whole stage of an axial compressor N Gourdain, S Burguburu, F Leboeuf, GJ Michon Computers & Fluids 39 (9), 1644-1655, 2010 | 101 | 2010 |
Comparison of RANS and LES for prediction of wall heat transfer in a highly loaded turbine guide vane N Gourdain, LYM Gicquel, E Collado Journal of propulsion and power 28 (2), 423-433, 2012 | 96* | 2012 |
A time-domain harmonic balance method for rotor/stator interactions F Sicot, G Dufour, N Gourdain | 94 | 2012 |
Prediction of the unsteady turbulent flow in an axial compressor stage. Part 1: Comparison of unsteady RANS and LES with experiments N Gourdain Computers & Fluids 106, 119-129, 2015 | 84 | 2015 |
Effect of tip clearance dimensions and control of unsteady flows in a multi-stage high-pressure compressor N Gourdain, F Wlassow, X Ottavy | 83 | 2012 |
Numerical simulation of rotating stall in a subsonic compressor N Gourdain, S Burguburu, F Leboeuf, H Miton Aerospace Science and Technology 10 (1), 9-18, 2006 | 76 | 2006 |
Steady/unsteady reynolds-averaged navier–stokes and large eddy simulations of a turbine blade at high subsonic outlet mach number T Léonard, LYM Gicquel, N Gourdain, F Duchaine Journal of Turbomachinery 137 (4), 041001, 2015 | 55 | 2015 |
Sustainable aviation in the context of the Paris Agreement: A review of prospective scenarios and their technological mitigation levers S Delbecq, J Fontane, N Gourdain, T Planès, F Simatos Progress in Aerospace Sciences 141, 100920, 2023 | 51 | 2023 |
Numerical analysis of the tip leakage flow field in a transonic axial compressor with circumferential casing treatment G Legras, N Gourdain, I Trebinjac Journal of Thermal Science 19, 198-205, 2010 | 43 | 2010 |
Chemical kinetics modeling and LES combustion model effects on a perfectly premixed burner G Albouze, T Poinsot, L Gicquel Comptes Rendus Mécanique 337 (6-7), 318-328, 2009 | 42 | 2009 |
Experimental and computational methods for flow investigation in high-speed multistage compressor X Ottavy, N Courtiade, N Gourdain Journal of propulsion and power 28 (6), 1141-1155, 2012 | 41 | 2012 |
Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on its test-rig—part I: rotating stall F Crevel, N Gourdain, S Moreau Journal of Turbomachinery 136 (10), 101003, 2014 | 38 | 2014 |
Towards massively parallel large eddy simulation of turbine stages G Wang, D Papadogiannis, F Duchaine, N Gourdain, LYM Gicquel Turbo Expo: Power for Land, Sea, and Air 55249, V06CT42A021, 2013 | 35 | 2013 |
Simulation numérique des phénomènes de décollement tournant dans les compresseurs axiaux N Gourdain Ecully, Ecole centrale de Lyon, 2005 | 32 | 2005 |
Prediction of the unsteady turbulent flow in an axial compressor stage. Part 2: Analysis of unsteady RANS and LES data N Gourdain Computers & Fluids 106, 67-78, 2015 | 31 | 2015 |